N7848A

Part: WEB — CRACKED (ZONE 500) · airframe 59,098 hrs · 33,833 cycles

LEFT WEB FITTING FOUND CRACKED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 58,555 hrs · 33,465 cycles

F/A REPORTS REAR PROVO DOOR L-2 SLIGHTLY HANGING OUT OF SHROUD. ADJUSTED GIRT BAR ASSY. FOR SECURED POSITION. OK FOR CONT. SERVICE REF.25-66-01 AMM

Part: LIGHT — FALSE INDICATION · airframe 56,667 hrs · 32,318 cycles

NOSE GEAR EXTENDED AND NOSE GEAR RED&GREEN LIGHTS ILLUMINATED WHEN GEAR HANDLE WAS MOVED TO OFF AFTER T/O DURING CLIMB. RAN QRH; NOSE GEAR RETRACTED; LIGHTS EXTINGUISHED; GEAR HANDLE LEFT IN UP POSITION <[01]. OK TO CONTINUE PER MEL 32-16-01. SP 1 C/W AUTH #242661.

Part: SKIN — CRACKED (ZONE 100) · airframe 56,208 hrs · 32,029 cycles

GROUND SERVICE DOOR SURROUND HAS CRACK AT BOTTOM<[01] INSPECTION C/W SURFACE INSPECTION OF CUT OUT PER NDT PART 6 51-00-00 PROCEDURE 4 NO DEFECTS NOTED;[02] REPAIRED GROUND SERVICE DOOR SURROUND PER SRM 53-10-15-2R-4;[03] INSPECTION C/W REPAIRED GROUND SERVICE DOOR SURROUND PER SRM 53-10-15-2R-4;[04] INSPECTION C/W REPAIRED GROUND SERVICE DOOR SURROUND PER SRM 53-10-15-2R-4

Part: MEGAPHONE — LOW (ZONE 200) · airframe 55,541 hrs · 31,593 cycles

CREW REPORTS AFT MEGAPHONE LOW<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-SWA-804-NG-01 (REMOVE AND REPLACE MEGAPHONE - PERMANENT)]

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 55,341 hrs · 31,461 cycles

AISLE EMERGENCY LIGHTS AT SEAT 6CBA & 9CBA INOP<[01] R\R M2335 BATTERY PACK IAW AMM 33-51-06.OPS CHECKED GOOD.

Part: OIL SYSTEM — LOW (APU) · airframe 55,284 hrs · 31,422 cycles

CLIMBING FL 360 APU FLAMED OUT WITH NO2 ENG IDG ON MEL LOST APU AT FL360<[01] FOUND APU OIL LEVEL LOW. SERVICED APU OIL PER AMM11-21-20. APU OPS CHECK GOOD.

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 55,243 hrs · 31,396 cycles

EMERGENCY BATTERIES PACKS M1675; M1688; M1672 FAIL TEST EMERGENCY BATTERIES PACKS M1675 M1688 M1672 FAIL TEST<[01] REPLACED EMERGENCY BATTERIES PACKS M1675; M1672; M1688; PERFORMED GOOD TEST PER AMM 33-51-06-960-805.<BR>TASK CARD COMPLETED;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

B.S. 663 VAPOR BARRIER IS CRACKED AT L.B.L. 45 W.L. 160.<[01] B.S. 663 VAPOR BARRIER DAMAGE AT L.B.L. 45 W.L. 160. HAS BEEN REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)].

Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 55,243 hrs · 31,396 cycles

FLIGHT DECK; P18 SUPPORT BRACKET BS259 SRT 8L CRACK<[01] REMOVED AND REPLACED BRACKET ON BS259 SRT 8L FLIGHT DECK; P18 I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G AND DWG141A0720.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: BRACKET — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION ON ACB BRACKET AT BS947.5 WL175 BL0.<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00VH4PU;[02] DISCREPANCY WILL NOT BE ACCOMPLISHED ON TTG8Q00VH4PU.;[03] REMOVED AND REINSTALLED ON ACB BRACKET AT BS 947.5 WL175 BL 0<BR>IAW SRM 51-40-02-0G-0 AND DWG# 147A9100 REV: A

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION ON ACB SIDEWALL SUPPORT BS727A+2; BS727A+18; BS727B+2; BS727B+6; BS727C+2; BS727C+10; BS727C+14; BS727D+3; BS727D+5; BS727D+18; BS727E+6; BS747+2; BS747+4; BS747+7 LBL 22 (MARKED)<[01] REMOVED AND INSTALLED NEW SIDEWALL SUPPORT BS727 TO BS847 LBL22 IAW SRM 51-40 -02 AND DWG146A7500 ID:0001 REV: B;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORRODED UPPER CHORD BAFFLE AFT CARGO DOOR SURROUND BS767+1.5; BS767+5.5; BS767+9; BS767+12; BS767+15.5 RBL21 (MARKED)<[01] REMOVED AND REPLACED FWD SHIELD LOWER ATTACH ANGLE IAW SRM 51-40-02 AND DWG 146A8123 ID:0016 REV -

Part: BAFFLE — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORRODED UPPER CHORD BAFFLE AFT CARGO DOOR SURROUND BS747+2; BS747+6; BS747+10; BS747+14; BS747+18 RBL22. UPPER CHORD BAFFLE ACB DOOR SURROUND BS747 TO BS767 WILL BE INSTALLED WITH THE FLOOR SIDEWALL SUPPORT ASSEMBLY ON CUSTOMER CARD NR TTG8Q00VH3YY. REJECTED. THERE IS NO REFERENCE FOR INSTALLATION OF A NEW UPPER CHORD BAFFLE FOR THE AFT CARGO DOOR SURROUND ON COMPLETED FAULT TTG8Q00VH3YY. UPPER BAFFLE AFT CARGO DOOR SURROUND REPLACED WITH FLOOR TO SIDEWALL SUPPORT ASSEMBLY ON CUSTOMER CARD TTG8Q00VH3YY STEP 2. SIDEWALL SUPPORT ASSEMBLY CAME WITH TWO BAFFLES INCLUDING THE MENTIONED ON THIS FAULT. FAULT TTG8Q00VH3YY WAS REPLACED THE FLOOR TO SIDEWALL SUPPORT INCLUDES NEW BAFFLE. THE BAFFLE IS REPLACED CONJUNCTION WITH FLOOR TO SIDEWALL SUPPORT ON CUSTOMER CARD TTG8Q00VH3YY. VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.

Part: DOOR SILL — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORRODED UPPER CHORD LOWER MAIN SILL AFT CARGO DOOR SURROUND BS767+4; BS767+5 RBL22 (MARKED)<[01] REMOVED AND REPLACED UPPER CHORD LOWER MAIN SILL AFT CARGO DOOR SURROUND FROM BS767 TO BS 787 RBL 22 IAW SRM 51-40-02 AND DWG 146A8123 ID:0017 REV: -

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION ON ACB ANGLE FLOOR SUPPORT AFT BULKHEAD BS 947 LBL 2; RBL10.75; RBL12.5; RBL15; RBL17.25; RBL20 WL 179 (MARKED)<[01] REMOVED AND REINSTALL ACB FLOOR SUPPORT AFT BULKHEAD ANGLE<BR>LBL 15 TO RBL 17 WL 179 BS 947 IAW SRM 51-40-02 AND DWG 147A7500 REV. C;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: STRAP — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORRODED STRAP LOWER MAIN SILL AFT CARGO DOOR SURROUND BS787+2 TO BS787+5 RBL 19.5 (MARKED)<[01] REMOVED AND REPLACED STRAP LOWER MAIN SILL AFT CARGO DOOR SURROUND IAW SRM 51-40-02 AND DWG 146A8120 ID: 0028 REV: -

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION ON ACB SIDEWALL SUPPORT BS747+16; BS747+17.5; BS767+3; BS767+10; BS767+10; BS767+14; BS767+18; BS787+1.5; BS787+10; BS787+18.5; BS807+2 LBL 22 WL 146.5 (MARKED)<[01] THIS TASK WAS COMPLETED IN CUSTOMER CARD TTG8Q00VH3X4.;[02] THIS FAULT WAS COMPLETED IN CUSTOMER CARD TTG8Q00VH3X4.;[03] CORROSION ON ACB SIDEWALL SUPPORT IS FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2; REMOVED AND REPLACED IS DOCUMENTED IN CUSTOMER CARD TTG8Q00VH3X4.;[04] VERIFIED ACTION 3.<BR>JOB COMPLETE.

Part: DOOR SILL — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORRODED UPPER CHORD LOWER MAIN SILL AFT CARGO DOOR SURROUND BS787+7.5; BS787+12.5; BS787+16.5; BS807+1.5; BS807+5; BS807+8.5; BS807+12.5; BS807+16; BS827+3.5; BS827+7 RBL19.5 (MARKED)<[01] REMOVED AND REPLACED WEB LOWER MAIN SILL AFT CARGO DOOR SURROUND<BR>BS794 TO BS847 RBL19.5 IAW SRM 51-40-02 AND DWG 146A8120

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION ON ACB SIDEWALL SUPPORT BS727+11; BS727+14.5; BS727+18; BS727A+2; BS727B+6; BS727B+10 RBL 22 (MARKED)<[01] REMOVED AND INSTALLED FLOOR TO SIDEWALL SUPPORT BS727 TO BS767 RBL 22 IAW SRM 51-40-02 AND DWG 146A7500 ID:0001 REV: B;[02] VERIFIED CORRECTIVE ACTION 1

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION ON ACB SIDEWALL SUPPORT BS727C+14; BS727D+10; BS727E+6; BS747 RBL 22 (MARKED)<[01] ACB SIDEWALL SUPPORT WILL BE REPLACED AND INSTALLED ON CUSTOMER CARD NBR: TTG8Q00VH3YY;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 160.<[01] REMOVED AND REPLACED B.S. 663 VAPOR BARRIER UPPER ATTACH <BR>BETWEEN LBL 6 TO LBL 65 WL 167.5 PER SRM 51-40-02; DWG 111A1000;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION FCB SIDEWALL SUPPORT BS 460+1.5; BS460+6.5; LBL 24 WL 156 (MARKED)<[01] REMOVED AND REPLACED FCB SIDEWALL SUPPORT BS395 TO BS500D LBL24 IAW SRM 51-40-02 AND DWG143A7500 ID:0058 R;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. COMPLETED WITH STEPS 1-7

Part: SUPPORT — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION FCB AFT SHIELD SUPPORT BS500+2 RBL 24.75 WL 156 (MARKED)<[01] REMOVED AND REPLACED FCB SHIELD SUPPORT<BR>BS500 TO BS 500A RBL 24.75 WL 156 IAW SRM 52-40-02-0G-0 <BR>AND DWG 143A0080<BR>CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CRACKED FCB BAFFLE BS 500+9 LBL 24.75 WL 156 (MARKED)<[01] REMOVED AND REPLACED BAFFLE AT FCB BETWEEN BS.500 - BS.500A LBL.24 WL 156 IAW SRM 51-10-02-05; SRM 51-40-02; & DWG#143A7505 REV: -;[02] VERIFIED CORRECTIVE ACTION ITEMS AND TASK CARD COMPLETED.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 45; W.L. 165.<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00VGMFZ;[02] REJECTED: STEP 1 NEEDS CORRECTED; #1 AMT BLOCK NEEDS CERTIFIED ON CARD TTG8Q00VGMFZ AND STEPS 3;4;5 CONTRADICT NEEDS CORRECTED.;[03] FIXED STEP 1; 3;4;5 ON COSTUMER CARD TTG8Q00VGMFZ<BR>THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00VGMFZ;[04] VERIFIED CORRECTION ACTION ITEM 3; STEP 1 COMPLETE; MEASUREMENT FIELD; CARD COMPLETE.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

PASSENGER CABIN; STRINGER CLIP CRACK AT STR6L; BS 727E<[01] REMOVED AND REPLACED STRINGER CLIP BETWEEN BS.727E; STR6L; IAW B-737-700 SRM 51-10-02; SRM 51-40-02 & DWG#146A1112 REV:;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.;[03] CARD COMPLETE.

Part: WEB — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORRODED ACB THRESHOLD WEB BS787+11; BS787+13; BS787+16; BS787+18.25; BS907+1; BS907+5.5; BS907+10; BS907+18.25; BS27+6; BS927+11 RBL25 WL 146.5 (MARKED)<[01] 01 - REMOVED AND INSTALLED NEW ACB THRESHOLD WEB BS794 TO BS847 RBL25 WL146.5 IAW SRM 51-40-02 AND DWG 146A8340.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION FCB TRACK TIEDOWN BS 400+1; BS420+16; BS480+16 LBL 18.25 WL 156 (MARKED)<[01] REMOVED AND REPLACED FCB TRACK TIEDOWN ASSY<BR>BS396-BS500D LBL 18.24 WL 156<BR>IAW SRM 51-40-02 & DWG 143A7500;[02] VERIFIED CORRECTIVE ACTION #1

Part: WEB — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION ON FCB THRESHOLD WEB AT BS440+5; BS440+8; BS440+12; BS440+15.5; BS460; BS460+1; BS 460+4; BS460+7; BS460+7; BS460+12.75; BS460+15.5; BS480+3.5. REMOVED AND REINSTALLED THRESHOLD WEB FCB <BR>IAW SRM 51-40-05 SRM 51-40-02 AND DWG 143A8120 REV: B;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-6

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8 W.L. 160.<[01] REMOVED AND REPLACED BS 663 VAPOR BARRIER UPPER ATTACH ANGLE RBL 8; WL 160 IAW DWG 111A1000; REV. B AND SRM 51-40-02.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CORROSION FCB SIDEWALL SUPPORT BS500A+2; BS500B+2; BS500B+6; BS500B+10; BS500B+14; BS500B+18; BS500C+2; BS500C+6; BSBS500C+10; BS+14 RBL 24.75 WL 156 (MARKED)<[01] UPDATED INSTALLED PARTS INFORMATION;[02] REMOVED AND REPLACED FCB SIDEWALL SUPPORT <BR>BS500A TO BS500D RBL 24.75 WL156 <BR>IAW SRM 51-40-02 & DWG 143A7501;[03] VERIFIED CORRECTIVE ACTION ENTRY 2.

Part: ANGLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CRACKED FCB ANGLE ATTACHED TO BAFFLE BS 400+1 LBL 24.75 WL 156 (MARKED)<[01] REMOVED AND REPLACED ANGLE ATTACHED TO BAFFLE BS 400+1 LBL 24.75 WL 156<BR>IAW SRM 51-40-02 & DWG 143A7505;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

HOLE ON FCB ANGLE SUPPORT BS 440+19 BETWEEN S-23L TO S-24L (MARKED)<[01] REMOVED AND REPLACED NEW ANGLE SUPPORT BS440+19 BETWEEN S-23L TO S-24L IAW SRM 51-40-02 AND DWG 417A2150 ID:0007 REV: B;[02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.;[03] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 55,243 hrs · 31,396 cycles

RH OVERWING EMERGENCY EXIT DOOR CUTOUT HAS CORROSION AT LOWER SILL STOP ANGLE BS616+13; RBL70 AND WL 208+14<[01] REMOVED AND REPLACED AT RH OVERWING EMERGENCY EXIT DOOR; SUPPORT ANGLE LOCATED BETWEEN BS 616 - BS. 636 RBL 70 WL 222 IAW B-737-700 SRM 51-10-02; SRM 51-40-02. AND DWG# 144A8201 REV: -;[02] VERIFIED CORRECTIVE ACTION 1.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CRACKED FCB ANGLE ATTACHED TO BAFFLE BS 500A+19 RBL 24 WL 156 (MARKED)<[01] REMOVED AND REPLACED ANGLE ATTACH ON BAFFLE BS500A+19 RBL24 IAW SRM 51-40-02 AND DWG 143A7505 ID:0006 REV:D;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-3

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

LEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CL BS540+6 LBL8. MARKED<[01] REMOVED AND INSTALLED NEW SUPPORT BRACKET AT ECS BAY; PER SRM 51-40-02 AND DWG: 212A1101; ID: 003;[02] REMOVED AND INSTALLED NEW SUPPORT BRACKET AT ECS BAY; PER SRM 51-40-02 AND DWG: 212A1101; REV -; ID: 003;[03] VERIFIED CORRECTIVE ACTION ENTRY 2.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 165.<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00VGMG1;[02] JOB COMPLETE.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

HOLE ON FCB ANGLE SUPPORT BS 400+19 BETWEEN S-22L TO S-23L (MARKED)<[01] REMOVED AND REPLACED ON FCB ANGLE SUPPORT BS400+19 BETWEEN S-22L TO S-23L IAW SRM 51-40-02 AND DWG 417A2150 ID: 0007 REV: B;[02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.;[03] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.

Part: ANGLE — CRACKED (ZONE 200) · airframe 55,243 hrs · 31,396 cycles

FWD SERVICE DOOR; CRACK ANGLE AT BS 294.5 STUB FRAME RBL 54 WL 208.1.<[01] REMOVED AND REPLACED CLIP (ANGLE) ON BS.294.5 RBL; 54 WL.208.1 IAW SRM 51-40-02 AND DWG# 141A8310 REV: B. AND REINSTALLED AND APPLIED SEAL AROUND FLOOR PANELS 222AF AND 222BF IAW B-737-700 AMM 53-21-00-400-801. USED Ï¿½Ï¿½TOOL GUN SCREW ID: ATS 1697. EXPIRATION DATE: 07/2025.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-4

Part: STRINGER — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<[01] REPAIRED STRINGER SECTION PER REF SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED RII STEP 7 COMPLETE.;[03] VERIFIED ALL STEPS COMPLETE; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD CARD COMPLETE.

Part: STRINGER — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R WL155. 'REPAIRED PER EA 24-153-02361. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-06.';[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: DRAIN MAST — CRACKED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

PANEL 194FL DRAIN MAST IS CRACKED NEAR UPPER AFT EDGE. (MARKED)<[01] REMOVED AND REPLACED

Part: SEAL — CRACKED (ZONE 300) · airframe 55,243 hrs · 31,396 cycles

LT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.

Part: PANEL — ELONGATED (ZONE 100) · airframe 55,243 hrs · 31,396 cycles

WING TO BODY FAIRING PANEL 194FR HAS ELONGATED HOLE (MARKED)<[01] REPAIRED DAMAGED FASTER HOLES ON WING TO BODY FAIRING PANEL 194FR IAW SRM 51-70-04-2R-9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: PANEL — PULLED (ZONE 600) · airframe 55,243 hrs · 31,396 cycles

R/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-9-A00753 (REPAIR 9 - REPAIR OF DAMAGE TO A FASTENER HOLE WITH LAMINATING RESIN AND CHOPPED FIBER - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION #1

Part: PANEL — PULLED (ZONE 500) · airframe 55,243 hrs · 31,396 cycles

L/W T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLE ON T/E OF PANEL (MARKED)<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-9-A00753 (REPAIR 9 - REPAIR OF DAMAGE TO A FASTENER HOLE WITH LAMINATING RESIN AND CHOPPED FIBER - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION #1

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 55,132 hrs · 31,323 cycles

AFT ENTRY DOOR EXTERNAL EMERGENCY LIGHT INOP<[01] RELAMPED IAW AMM 33-51-04

Part: GIRT BAR — OUT OF POSITION (R2 DOOR) · airframe 54,898 hrs · 31,198 cycles

R EMER ESCAPE. SLIDE GIRT BAR RING RECENTS SLIDE FROM BEING ARMED.<[01] REPOSITIONED & SECURED R2 GIRT BAR RING. SLIDE ARMS NORMAL REF AMM 25-66-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,188 hrs · 30,761 cycles

ROW 8 FED EMERGENCY LIGHT INOP<[01] RELAMPED ROW 8 FED EMERGENCY AREA LIGHT PER AMM 33-51-03. OPS CHECK GOOD.

Part: PANEL — CRACKED (BS 540 RBL 23) · airframe 53,973 hrs · 30,617 cycles

BREAK ASSY PANEL AT BS 540 -RBL 23 CRACKED ;IN DISTRIBUTION BAY<[01] 01 - REMOVED AND REPLACED BREAK PANEL ASSY PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 52,204 hrs · 29,530 cycles

R1; ROW 6DEF AND L1 EXIT SIGN E LIGHTS OUT.<[01] R/R BATTERY PACK (M1674) IAW AMM 33-51-06.

Part: HANDLE — LOOSE (ZN 200 FUS TOP) · airframe 51,985 hrs · 29,370 cycles

FWD ENTRY DOOR HANDLE LOOSE<[01] FOUND FWD ENTRY HANDLE BOLTS LOOSE; SECURED IN REF TO AMM 52-11-31

Part: SEAT BACK — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 50,682 hrs · 28,518 cycles

SEAT 11E RECLINES IN FRONT OF EXIT ROW<[01] ADJUSTED SEAT LOCK ASSEMBLY ON SEAT 11E PER CMM 25-21-42.

Part: HANDLE — DETACHED (LT OVERWING) · airframe 50,106 hrs · 28,143 cycles

L OVERWING EMERGENCY EXIT LOWER DOOR HANDLE DETACHED<[01] SECURED PER SIP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,040 hrs · 28,102 cycles

AFT ENTRY AND ROW LOCATION 20ABC EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK FROM M1673 POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD.

Part: NONE — FAILED (#2 ENGINE) · airframe 49,251 hrs · 27,592 cycles

#2 ENGINE OVER TEMP ON CLIMB AT 1000 FT. MAX TEMP NOTED 939 C FOR 10-15 SECONDS / [01] PERFORMED ENGINE BOROSCOPE OF #2 ENGINE HIGH PRESSURE TURBINE AND ALL STAGES OF LOW PRESSURE TURBINES AS PER AMM 72-00-00-200-807-F00 AND 72-00-00-200-808-F00. NO DEFECTS NOTED. PERFORMED IDLE LEAK CHECK OF DRIVE PAD. NO LEAKS NOTED.;[02] PERFORMED ENGINE BOROSCOPE OF #2 ENGINE HIGH PRESSURE TURBINE AND ALL STAGES OF LOW PRESSURE TURBINES AS PER AMM 72-00-00-200-807-F00 AND 72-00-00-200-808-F00. NO DEFECTS NOTED. PERFORMED IDLE LEAK CHECK OF DRIVE PAD. NO LEAKS NOTED.;[03] PERFORMED FIM TASK 73-11-801 AND. FILM 77-21-801 FOUND S1 FAILED R&R CJ9 HARNESS PER AMM 73-21-06; PERFORMED ENGINE BOROSCOPE OF #2 ENGINE HIGH PRESSURE TURBIN AND ALL STAGES OF LOW PRESSURE TURBINES AS PER AMM 72-00-00-200-807-F00 AND 72-00-00-200-808-F00. NO DEFECTS NOTED. PERFORMED IDLE LEAK CHECK OF DRIVE PAD; NO LEAKS NOTED. PERFORMED AMM 71-00-00-700-813-F00 TEST 5 POWER ASSURANCE NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,870 hrs · 27,337 cycles

PASSENGER CABIN ROW 1 CEILING EMERGENCY LIGHT INOP. / [01] RELAMPED PASSENGER CABIN ROW 1 CEILING EMERGENCY LIGHT AS PER REF B737 AMM 33-51-03-960-801. TEST OK.;[02] VERIFIED STEP 1.

Part: BATTERY PACK — INOPERATIVE (AFT CABIN) · airframe 48,870 hrs · 27,337 cycles

EMERGENCY LIGHTS INOP FOR BATTERY PACK M1670 AT STA. 727C / [01] REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK M1670 AT STA. 727C; AS PER REFERENCE B737 AMM 33-51-06-960-805 AND AMM 33-51-06-960-806.PERFORMED OPERATIONAL TEST EMERGENCY LIGHTS; TEST NORMAL OPERATION.;[02] VERIFIED STEP 1

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 48,870 hrs · 27,337 cycles

AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED / [01] RECEIVED REPAIRED SCUFF PLATE P/N: 146A8341-9 PO# 1772343<BR>REF. TASK CARD TTG8Q004FMRX FOR INSTALLATION;[02] VERIFIED 1

Part: NONE — CORRODED (AFT CARGO) · airframe 48,870 hrs · 27,337 cycles

' CORROSION' AFT CARGO COMPARTMENT RH STA 727B TO 727C STR25R Z-CHANNEL SPOTS OF CORROSION / [01] FOUND EXFOLIATED CORROSION AT AFT CARGO COMPT RH STA 727B TO 727C STR25R Z-CHANNEL OUT OF LIMITS PER REF B737-700 SRM 51-10-02-0G-0;[02] VERIFIED 1;[03] CUT AND REMOVED DAMAGE AT AFT CARGO COMPT R/H ZEE CHANNEL STR25R FROM STA 727 TO STA 727B +12' PER REF B737-700 SRM 53-00-53-2R-5;[04] VERIFIED 3. OK TO LOCATE AND DRILL HOLES;[05] FABRICATED AND LOCATED AND DRILLED NEW REPAIR SPLICE AND ZEE CHANNEL SECTION FROM STA 727 TO 727B +12' AT AFT CARGO COMPT STR25R PER REF B737-700 SRM 53-00-53-2R-5;[06] VERIFIED STEP 5<BR>OK TO TREAT AND PRIME PARTS;[07] TREATED AND PRIMED SPLICER AND AREA AT AFT CARGO COMPT RH ZEE CHANNEL FROM STA 727 TO STA 727B+12' PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804.;[08] TREATED AND PRIMED SPLICER AND AREA AT AFT CARGO COMPT RH ZEE CHANNEL FROM STA 727 TO STA 727B+12' PER B737-700 AMM 51-21-72-370-804 AND SRM 51-20-01-0G-0;[09] VERIFIED 8.;[10] INSTALLED NUTPLATES IN RH ZEE CHANNEL FROM STA 727 TO 727B +12' PER REF B737-700 SRM 51-40-02-0G-0;[11] VERIFIED 10;[12] OK TO INSTALL REPAIR;[13] INSTALLED REPAIR SPLICE PER REF B737-700 SRM 51-40-02-0G-0;[14] INSTALL REPAIR PER SRM 53-00-53-2R-5 AND SRM 51-40-02-0G-0;[15] VERIFIED 14;[16] C/W

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

CRACK FOUND AT UPPER HOLE OF STUB FRAME (I/B) AT R-1 DOOR CUT OUT IAW NDTM PART 6.51-00-00 PROCEDURE 16. CRACK IS AT 5 O'CLOCK POSITION .CRACK LENGTH 0.020' CRACK FOUND AT UPPER HOLE OF STUB FRAME (I/B) AT R-1 DOOR CUT OUT IAW NDTM PART 6.51-00-00 PROCEDURE 16. CRACK IS AT 5 O&#39;CLOCK POSITION .CRACK LENGTH 0.020&#34; / [01] APPLIED PAINT STRIPPING AT R-1 DOOR FWD UPPER JAMB OUTER SKIN PER B737-700 51-21-11-150-810.;[02] VERIFIED 1;[03] REMOVED STUB FRAME FROM FWD JAMB UPPER R-1 DOOR DOOR CUT OUT PER B737-700 SRM 51-40-02-0G-0.;[04] LOCATED AND PARTIALLY DRILL HOLES AT UPPER STUB FRAME PER SRM 51-10-02-0G-0;[05] COMPLETED DRILLED EXITING HOLES AT NEW STUB FRAME PER SRM 51-40-02-0G-0 AND 51-40-05-0G-0;[06] VERIFIED 3; 4 & 5;[07] OK TO TREAT AND PRIME FASTENER'S HOLES;[08] TREAT; PRIMER TOP COAT PER SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804;[09] VERIFIED 8. OK TO INSTALL STUB FRAME;[10] MIXED BMS 5-95 SEALANT AT 7:30 AM 08-15-2022. SQUEEZE OUT TIME BY 3:30 PM 08-18-2022.;[11] PARTIALLY INSTALLED STUB FRAME AND DEPRESSOR ON R-1 DOOR FWD JAMB UPPER SIDE. PER SRM 51-40-02-0G-0; AND DWG 141A8370.;[12] VERIFIED 10 AND 11;[13] COMPLETED INSTALLATION OF STUB FRAME AND DEPRESSOR ON R-1 DOOR FWD JAMB UPPER SIDE. PER SRM 51-40-02-0G-0; AND DWG 141A8370.

Part: SIGN — CRACKED (FWD CABIN) · airframe 48,870 hrs · 27,337 cycles

EXIT SIGN AT FWD GALLEY G1 AND LAV A BASE IS CRACKED / [01] REMOVED AND REPLACED EXIT SIGN AT FWD GALLEY G1 AND LAV A BASE REF: 35-51-01-960-802;[02] VERIFIED 1

Part: FITTING — CRACKED (L//H WING) · airframe 48,870 hrs · 27,337 cycles

LEFT WING REAR SPAR INB LOWER FIXED T/E O/B FLAP TRACK NO-3 WIGGLE FITTING CRACKED MKD DOT / [01] REMOVED AND REPLACED WIGGLE FITTING AT LEFT WING REAR SPAR INB LOWER FIXED T/E OB/ FLAP TRACK NO. 3 AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.

Part: NONE — CRACKED (FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

FWD CABIN CTR AISLE FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACKED @ RBL 10 BETWEEN. STA 380 AND 400 / [01] REMOVED FWD CABIN CTR AISLE FLOOR SUPPORT INTERCOASTAL UPPER CAP @ RBL 10 BETWEEN STA 380 AND 400 IAW 737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW HOLES ON INTERCOSTAL UPPER CAP PER SRM 51-40-05-0G-0.;[03] VERIFIED 2. OK TO INSTALL;[04] INSTALLED FWD CABIN CTR AISLE FLOOR SUPPORT INTERCOASTAL UPPER CAP @ RBL 10 BETWEEN STA 380 AND 400. PER SRM 51-40-02-0G-0.;[05] VERIFIED 4

Part: INTERCOSTAL — CRACKED (FWD FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ RBL 17 BETWEEN. STA 312 AND 328 MKD DOT / [01] REMOVED FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ RBL 17 BETWEEN. STA 312 AND 328 IAW 737-700 AMM 51-40-02-0G-0;[02] REMOVED FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ RBL 17 BETWEEN. STA 312 AND 328 IAW 737-700 SRM 51-40-02-0G-0;[03] VERIFIED 2;[04] LOCATED AND DRILLED NEW FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ RBL 17 BETWEEN. STA 312 AND 328 IAW 737-700 SRM 51-40-05-0G-0;[05] VERIFIED STEP 4; OK TO TREAT AND PRIME HOLE LOCATIONS;[06] TREATED AND PRIMED DRILLED HOLES ON FLOOR SUPPORT INTERCOSTAL AS PER B737-700 AMM 51-21-41-370-803 AND 51-21-72-370-804;[07] VERIFIED STEP 6; OK TO INSTALL NEW INTERCOSTAL;[08] INSTALLED NEW INTERCOASTAL AT FWD CABIN WET AREA FLOOR SUPPORT @ RBL 17 BETWEEN. STA 312 AND 328 IAW 737-700 SRM 51-40-02-0G-0;[09] VERIFIED 8

Part: FRAME — CRACKED (FWD FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

FWD CABIN WET AREA L/H SIDE FUS. SUPPORT FRAME SMALL CRACKED @ FLANGE CUTOUT ABOVE L-1 DOOR CUTOUT FWD STA 312 MKD DOT / [01] WORK ACCOMPLISHED ON TTG8Q00DY05V;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (FWD FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

FWD CABIN CTR AISLE FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACKED @ LBL 13 BETWEEN. STA 380 AND 400 / [01] REMOVED FWD CABIN CTR AISLE FLOOR SUPPORT INTERCOSTAL UPPER CAP @ LBL 13 BETWEEN. STA 380 AND 400 IAW B737-700 SRM 51-40-02-0G-9;[02] LOCATED AND DRILLED NEW HOLES ON INTERCOSTAL UPPER CAP PER SRM 51-40-05-0G-0.;[03] VERIFIED 2. OK TO INSTALL;[04] VERIFIED 2. OK TO INSTALL;[05] INSTALLED FWD CABIN CTR AISLE FLOOR SUPPORT INTERCOSTAL UPPER CAP PER SRM 51-40-02-0G-0.;[06] VERIFIED 5

Part: INTERCOSTAL — CRACKED (FWD FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

FWD WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ FASTENER HOLE LBL 13 BETWEEN. STA 344 AND 360 MKD DOT / [01] REMOVED FWD WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ FASTENER HOLE LBL 13 BETWEEN. STA 344 AND 360 IAW B737-700 SRM 51-40-02-0G-0;[02] VERIFIED 1;[03] LOCATED AND DRILL NEW INTERCOSTAL REFERENCE B737-700 SRM 51-40-05-0G-0;[04] VERIFIED STEP 3<BR>OK TO INSTALL INTERCOSTAL;[05] INSTALLED NEW INTERCOSTAL BETWEEN STA. 344 AND 360 LBL 13' FWD WET AREA REFERENCE B737-700 SRM 51-40-02-0G-0;[06] VERIFIED 5

Part: FLOOR PANEL — CRACKED (AFT FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

AFT CABIN WET AREA FLOOR PANEL # 241ADF CRACKED @ AFT O/B CORNER MKD DOT / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON FLOOR PANEL AND FOUND PANEL OUT OF LIMITS PER B737 NDTM 51-05-01;[02] RECIEVED NEW PANEL 241ADF P/N: 815A0044-1 PO# 1772343.;[03] VERIFIED STEPS #1 AND #2

Part: FITTING — CORRODED (FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

CORROSION ** FWD CABIN WET AREA L1 DOOR LOWER SILL INNER CHORD AFT SLIDE LATCH FITTING FASTENERS HOLES / [01] REMOVED CORROSION ON LATCH FITTING AT FWD CABIN WET AREA L1 DOOR LOWER SILL INNER CHORD AFT SLIDE PER B737-700 SRM 51-10-02-0G-0.;[02] VERIFIED 1;[03] ADD TO STEP 1. EXFOLIATED CORROSION FOUND AROUND FASTENER HOLES;[04] VERIFIED 3. OK TO INSTALL NEW TIEDOWN( LATCH FITTING);[05] INSTALLED NEW TIEDOWN ( LATCH FITTING ) AT FWD CABIN WET AREA L1 DOOR LOWER SILL INNER CHORD AFT SLIDE FITTING PER B737-700 SRM 51-40-02-0G-0.;[06] VERIFIED 5

Part: INTERCOSTAL — CRACKED (FWD FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ LBL 48 BETWEEN. STA 312 AND 328 MKD DOT / [01] REMOVED FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL @ LBL 48 BETWEEN. STA 312 AND 328 IAW B737-700 AMM 51-40-02-0G-0;[02] REMOVED FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL @ LBL 48 BETWEEN. STA 312 AND 328 IAW B737-700 SRM 51-40-02-0G-0;[03] VERIFIED 2;[04] LOCATED AND DRILLED FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL @ LBL 48 BETWEEN. STA 312 AND 328 IAW B737-700 SRM 51-40-05-0G-0;[05] VERIFIED STEP 4; OK TO TREAT AND PRIME HOLES;[06] TREATED AND PRIMED NEW FLOOR SUPPORT INTERCOSTAL AS PER B737-700 AMM 51-21-41-370-803 AND 51-21-72-370-804;[07] VERIFIED STEP 6; OK TO INSTALL NEW INTERCOSTAL;[08] INSTALLED NEW INTERCOASTAL AT FWD CABIN WET AREA FLOOR SUPPORT @ LBL 48 BETWEEN. STA 312 AND 328 IAW 737-700 SRM 51-40-02-0G-0;[09] VERIFIED 8

Part: NONE — CRACKED (FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

MAIN CABIN CENTER WING BOX FLOOR SUOOPRT BREAK CRACKED @ STA 540 RBL 1 MKD DOT / [01] REMOVED FLOOR SUPPORT IAW SRM 51-40-02-0G-0;[02] CORRECTION TO STEP 1; REMOVED FLOOR SUPPORT AT MAIN CABIN CENTER WING BOX ON STA 540 RBL 1 PER B737-700 SRM 51-40-02-0G-0.;[03] ADD TO STEP 2: FLOOR SUPPORT BREAK.;[04] VERIFIED REMOVED FLOOR SUPPORT BREAK. (STEP 2 WITH CORRECTION 3). OK TO INSTALL NEW SUPPORT BREAK;[05] INSTALLED NEW SUPPORT BREAK AT MAIN CABIN CENTER WING BOX ON STA 540 RBL 1 PER B737-700 SRM 51-40-02-0G-0.;[06] VERIFIED 5

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

FWD CABIN WET AREA L1 DOOR LOWER SILL INNER CHORD AFT FLOOR PANEL END BROKEN AROUND SLIDE LATCH FITTING STA 344 / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON FLOOR PANEL AND FOUND PANEL OUT OF LIMITS PER B737 NDTM 51-05-01;[02] RECIEVED NEW FLOOR PANEL P/N:141A5810Y183 PO#1781750. REF. TASK CARD TTG8Q00CW91T FOR CLOSING;[03] INSTALLED FLOOR PANEL PER TASK CARD TTG8Q00CW91T;[04] VERIFIED 1; 2 AND 3

Part: INTERCOSTAL — CRACKED (FWD FUSELAGE) · airframe 48,870 hrs · 27,337 cycles

FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ BL-0 BETWEEN. STA 277 AND 294.5 MKD DOT / [01] REMOVED FWD CABIN WET AREA FLOOR SUPPORT INETERCOASTAL BL-0 BETWEEN STA 277 AND 294.5 IAW B737-700 SRM 51-40-02-0G-0;[02] VERIFIED 1;[03] LOCATED AND DRILLED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA AT BL0 BETWEEN STA 277 AND 294.5 B737-700 SRM 51-40-05-0G-0;[04] VERIFIED 3. OK TO TREAT AND PRIME;[05] TREATED AND PRIMED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA AT BL0 BETWEEN STA 277 AND 294.5 B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[06] VERIFIED 5;[07] INSTALLED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA AT BL0 BETWEEN STA 277 AND 294.5 B737-700 SRM 51-40-02-0G-0

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 48,870 hrs · 27,337 cycles

FWD CARGO DOOR CUTOUT CENTRAL SCUFFPLATE CRACKED FWD EDGE / [01] COMPLETED TABLE MEASUREMENTS;[02] RECEIVED REPAIRED SCCUFF PLATE<BR>REF. TASK CARD TTG8Q004FS5V FOR SCUFF PLATE INSTALLATION;[03] VERIFIED; STEPS # 1 AND 2.<BR>REF. TASK CARD TTG8Q004FS5V FOR SCUFF PLATE INSTALLATION

Part: FITTING — CRACKED (R/H WING) · airframe 48,870 hrs · 27,337 cycles

R/W REAR SPAR DEFLECTION CONTROL RIB FIXED PANEL LOWER VERTICAL SEAL FITTING CRACKED INB SIDE MKD DOT / [01] LOCATED AND DRILLED FITTING AS PER B737-700 SRM 51-40-05-0G-0;[02] LATE ENTRY: REMOVED FITTING AT RT WING REAR SPAR DELFECTION CONTROL RIB LOWER VERTICAL FITTING AS PER B737-700 SRM 51-40-02-0G-0;[03] VERIFIED STEPS 1 AND 2<BR>OK TO INSTALL;[04] INSTALLED NEW FITTING AT REAR SPAR DEFLECTION CONTROL RIB FIXED AS PER B737-700 SRM 51-40-02-0G-0;[05] VERIFIED STEP 4

Part: BRACKET — CRACKED (R/H WING) · airframe 48,870 hrs · 27,337 cycles

RIGHT WING TO BODY FAIRING 191AR SUPPORT CRACKED AT WING L/E ATTACH POINT.(51-003) / [01] REMOVED RIGHT WING TO BODY FAIRING 191AR SUPPORT BRACKET AT WING L/E ATTACH POINT PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED 1;[03] REMOVED PANEL #195AR AND PANEL #191FR FOR ACCESS TO SUPPORT BRACKET PER B737-700 SRM 51-40-02-0G-0.;[04] VERIFIED 2;[05] LOCATED AND DRILLED NEW RIGHT WING TO BODY FAIRING 191AR SUPPORT BRACKET AT WING L/E ATTACH POINT PER B737-700 SRM 51-40-05-0G-0.;[06] VERIFIED 5;[07] OK TO TREAT AND PRIMER;[08] TREATED AND PRIMED HOLES ON RIGHT WING TO BODY FAIRING 191AR SUPPORT BRACKET AT WING L/E ATTACH POINT AS PER B737-700 AMM 51-21-41-370-803 AND 51-21-72-370-804;[09] OK TO INSTALL SUPPORT AT RIGHT WING TO BODY FAIRING (191AR PANEL);[10] INSTALLED RIGHT WING TO BODY FAIRING 191AR SUPPORT AT WING L/E ATTACH POINT AS PER B737-700 SRM 51-40-02-0G-0;[11] VERIFIED STEP#10. OK TO INSTALL PANELS 195AR; 191FR AND 191AR.;[12] INSTALLED PANEL'S NUMBER 195AR; 191FR AND 191AR PER B737-700 SRM 51-40-02-0G-0.;[13] VERIFIED 12. PENDING SEALANT PANEL 191AR;[14] APPLIED SEALANT TO PANEL NUMBER 191AR PER B737-700 AMM 51-31-00-390-804.;[15] VERIFIED 14

Part: PANEL — ELONGATED (R/H WING) · airframe 48,870 hrs · 27,337 cycles

RIGHT WING LWR PANEL 661CB HAS ELONGATED/ CRACKED HOLES. CORRECT PANEL IS 621CB / [01] PERFORMED VISUAL INSPECTION AND TAP-TEST INSPECTION AT ACCESS PANEL 661CB; ELONGATED HOLES FOUND; NO WATER NOTE AND NO DELAMINATION FOUND. REF B737-700 SRM 51-70-04-2R-9 PARAGRAPH 4 A AND NDT PART 1 51-05-01 PARAGRAPH 5.;[02] PREPARED AREA TO FILL DAMAGES HOLES WITH A MIXTURE OF LAMINATING RESIN AND CHOPPED FIBER. REF B737-700 SRM 51-70-04-2R-9 PARAGRAPH 4 C.;[03] OK TO INSTALL REPAIR;[04] REPAIRED ALONGATED HOLES AT ACCESS PANEL 661CB. REF B737-700 SRM 51-70-04-2R-9 PARAGRAPH 4 D;E.F.G;H;I;J;K;L AND M. MATERIAL USED FIBERGLASS REPAIR FABRIC PO#:1690463 AND RESIN PO#:1778994;[05] VERIFIED 4;[06] APPLIED TOPCOAT TO REWORKED AREA AS PER B737-700 AMM 51-21-73-370-804;[07] CORRECT PANEL IDENTIFICATION IS 621CB;[08] VERIFIED STEPS 6 AND 7

Part: HOOK — LOOSE (R1 DOOR) · airframe 47,376 hrs · 26,403 cycles

FWD SVC DOOR GIRT BAR LOOSE IN STORAGE HOOKS ; / [01] ADJ. GIRT BAR HOOKS PER SIP

Part: PANEL — ELONGATED (FUSELAGE) · airframe 47,189 hrs · 26,296 cycles

CENTER WHEEL WELL PANEL 193D HAS ELONGATED FASTENER HOLES. ; / [01] REPLACED 193D PANEL WITH SERVICEABLE PANEL

Part: PANEL — ELONGATED (FUSELAGE) · airframe 47,189 hrs · 26,296 cycles

AFT WING-TO-BODY FAIRING PANEL 194E HAS ELONGATED FASTENER HOLES. ; / [01] PREPPED PANEL 193D; NEEDS SEAL INSTALLED AND PAINT; [02] REMOVED AN REPLACE PANEL PER AMM 53-51-21

Part: SIGN — LOOSE (CABIN) · airframe 45,356 hrs · 25,200 cycles

EXIT SIGN FELL OFF FO'S SIDE OVERWING EMER. EXIT. INSTALLED LOOSE OVERWING EXIT SIGN IAW AMM 20-00-00

Part: GIRT BAR — LOOSE (CABIN L2 DOOR) · airframe 44,568 hrs · 24,755 cycles

CUSTOMER WALK- PAX CABIN L2 DOOR AFT GIRT BAR FITTING LOOSE. RESECURED FASTENERS AT L2 DOOR AFT GIRT BAR FITTING AS PER B737 AMM 25-66-02-400-801.

Part: SKIRT — OUT OF POSITION (R2 DOOR SLIDE) · airframe 44,568 hrs · 24,755 cycles

R2 DOOR SLIDE SKIRT TOUCHING SCUFF PLATES. REPOSITIONED R2 DOOR SLIDE SKIRT REF B737-700 AMM 25-66-00-440-801.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

AFT CARGO FLOOR STRUCTURE RAIL AT RBL-3 AND STA 727E BENT, AFT CARGO FLOOR STRUCTURE RAIL AT STA 727E RBL WAS FOUND CRACKED. PERFORMED FLOOR BEAM REPAIR AS PER B737-700 SRM 53-00-53-2R-4 REPAIR 4 FIG 201 BETWEEN STA 727E-STA 747 RBL 3.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CORROSION AFT CARGO FLOOR STRUCTURE TIE DOWN TRACK UPPER SURFACE WITH CORROSION SPOTS AT RBL-13.84 BETWEEN STA-787 TO 847. REMOVED AND REPLACED TIE DOWN TRACK SECTION FROM STA 755 TO 887 RBL 13.85 AS PER REF B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND TIE DOWN TRACK PN 654A0004.35 TRACK SPLICE BPC 1509-10068.

Part: SCUFF PLATE — CRACKED (FWR CARGO BAY) · airframe 44,568 hrs · 24,755 cycles

FORWARD CARGO DOOR AFT SCUFF PLATE HAS A CRACK. REPAIRED FWD CARGO DOOR AFT SCUFF PLATE PER B737-700 SRM 53-30-15-2R1 REPAIR 1 WELDING REPAIR WAS ACCOMPLISHED BY OUTSIDE VENDOR PO 412863

Part: FLOOR PANEL — DISINTEGRATED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CABIN FLOOR PANEL 241FF TOP LAYER DISINTEGRATING. CLEANED AND REPAIRED MAIN CABIN FLOOR PANEL 241FF TOP LAYER AS PER BOEING 737 SRM 53-00-50-2R-1. MATERIAL USED PO 1480720.

Part: FLOOR PANEL — DISINTEGRATED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CABIN FLOOR PANEL 232RF TOP LAYER DISINTEGRATING. CLEANED & REPAIRED MAIN CABIN FLOOR PANEL 232RF TOP LAYER AS MARKED AS PER B737 SRM 53-00-50-2R-1 MATERIALS USED PO 1480720 & PO 1671335.

Part: FLOOR PANEL — DISINTEGRATED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CABIN FLOOR PANEL 242CF TOP LAYER DISINTEGRATING. CLEANED & REPAIRED MAIN CABIN FLOOR PANEL 242CF TOP LAYER AS MARKED AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO 1480720 AND PO 1671335.

Part: FLOOR PANEL — DETERIORATED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CABIN FLOOR PANEL 231YF TOP LAYER DISINTEGRATING. CLEANED & REPAIRED MAIN CABIN FLOOR PANEL 231YF TOP LAYER AS MARKED AS PER B737 SRM 53-00-50-2R-1 MATERIALS USED PO 1480720 AND PO 1671335.

Part: FLOOR PANEL — DISINTEGRATED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CABIN FLOOR PANEL 241EF TOP LAYER DISINTEGRATING. CLEANED AND REPAIRED MAIN CABIN FLOOR PANEL 241 EF TOP LAYER AS MARKED AS PER B737 SRM 53-00-50-2R-1. MATERIALS USED PO 1480720 AND PO 1671335.

Part: FLOOR PANEL — DISINTEGRATED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CABIN FLOOR PANEL 232SF TOP LAYER DISINTEGRATING. CLEANED AND REPAIRED MAIN CABIN FLOOR PANEL 232SF TOP LAYER AS MARKED AS PER B737 SRM 53-00-50-2R-1. MATERIAL USED PO 1480720 AND PO 1671335.

Part: FLOOR PANEL — DISINTEGRATED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CABIN FLOOR PANEL 242DF TOP LAYER DISINTEGRATING. CLEANED AND REPAIRED MAIN CABIN FLOOR PANEL 242DF TOP LAYER AS MARKED AS PER B737 SRM 53-00-50-2R-1 MATERIALS USED PO 1480720 AND PO 1671335.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

L1 ENTRY DOOR FWD CUTOUT SURROUNDING FRAME HAS 5EA RUBBER NUTS DAMAGED TREADS MKD DOTS 60035 REMOVED AND REPLACED AT L1 ENTRY DOOR FWD CUT-OUT IAW B737700 SRM 5140020G0 ALL RUBBER NUTPLATES (SHOCK MOUNTS)

Part: PLATE — CORRODED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

** CORROSION ** AFT CARGO COMPARTMENT FLOOR DOOR CUTOUT LOWER JAMB FWD AND AFT PLATES MKD DOTS 60-026 / REMOVED CORROSION ON AFT CARGO COMPARTMENT FLOOR CUT OUT LOWER JAMB FWD AND AFT PLATES IN REF B737-700 SRM 51-10-02-0G-0. CORROSION PASSES ALL THE WAY THRU MATERIAL FOUND OUT OF LIMITS IN REF B737-700 SRM 53-00-53-1A-1. REPLACED AFT CARGO COMPARTMENT FLOOR DOOR CUT OUT LOWER JAMB FWD AND AFT PLATES IN REF B737-700 IPC 25.52.10.02 DETAILS F AND G

Part: FLOOR PANEL — DISINTEGRATED (FUSELAGE) · airframe 44,568 hrs · 24,755 cycles

CABIN FLOOR PANEL 231ZF TOP LAYER DISINTEGRATING. CLEANED AND REPAIRED MAIN CABIN FLOOR PANEL 231ZF TOP LAYER AS MARKED AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO 1480720 AND PO 1671335.

Part: FITTING — CRACKED (RT WING) · airframe 44,568 hrs · 24,755 cycles

RIGHT WING REAR SPAR DEFLECTION CONTROL RIB PANEL VERTICAL SEAL FITTING CRACKED OUB MKD DOT 60-023 / REMOVED VERTICAL SEAL FITTING AT RIGHT WING REAR SPAR DEFLECTION CONTROL RIB IAW B737-700 SRM 51-40-02-0G-0 AND INSTALLED VERTICAL FITTING ASSY NEW AT RIGHT WING REAR SPAR DEFLECTION CONTROL RIB IAW B737-700 SRM 51-40-02-0G-0

Part: RIB — LOOSE (R/H WING) · airframe 44,568 hrs · 24,755 cycles

RIGHT WING REAR SPAR DEFLECTION CONTROL RIB PANEL OUB. ATTACHED FITTING LOOSE APPEAR CORROSION MKD DOT 60-022 / REMOVED AND INSTALLED T/E SUPPORT BEAM AT RIGHT WING REAR SPAR DEFLECTION CONTROL RIB AND APPLIED TREATED; PRIMED AND PAINTED IAW B737-700 SRM 51-40-02-0G-0; SRM 57-51-02-2R-4. SRM 51-20-01-0G-0 AND SRM 51-21-72-370-804

Part: RIB — CRACKED (LT HORIZ STAB LE) · airframe 44,568 hrs · 24,755 cycles

LEFT STAB L/E PANEL; NR 4 RIB FROM IB IS CRACKED. REMOVED AND REPLACED NR 4 RIB AT LT HORIZONTAL STAB LE AS PER REF B737-700 SRM 51-40-02-0G-0 AND DWG 186A1001.

Part: HOUSING — CRACKED (LT OVERWING DOOR) · airframe 44,568 hrs · 24,755 cycles

L/H OVERWING HATCH LOWER STRAP HOUSING CRACKED / REMOVED AND REPLACED L/H OVERWING HATCH LOWER STRAP HOUSING AS PER B737-7 AMM 52-22-51-000-801 AMM 52-22-51-400-801

Part: FITTING — CRACKED (LT WING) · airframe 44,568 hrs · 24,755 cycles

LEFT WING REAR SPAR T/ E DEFLECTION CONTROL RIB PANEL WEB SEAL FITTING CRACKED INB MKD DOT 60-013 / REMOVED AND INSTALLED WEB SEAL FETTING AND WEB AT LEFT WING SPAR T/E DEFLECTION CONTROL RIB IAW B737-700 51-40-02-0G-0

Part: HOUSING — CRACKED (RT OVERWING DOOR) · airframe 44,568 hrs · 24,755 cycles

R/H OVERWING HATCH LOWER STRAP HOUSING CRACKED / REMOVED AND REPLACED RH OVERWING HATCH LOWER STRAP HOUSING AS PER B737-700 AMM 52-22-51-000-801 AMM 52-22-51-400-8001

Part: PRESSURE DECK — DAMAGED (COCKPIT) · airframe 44,568 hrs · 24,755 cycles

FLIGHT DECK FLOOR DAMAGED IN 2 AREAS BS 260. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR, PER EA 1-A53-33179 REV 1

Part: LENS — CRACKED (CABIN) · airframe 44,338 hrs · 24,620 cycles

AFT SERVICE DOOR EXIT LIGHT LENS CRACKED REPLACED AFT SERVIE DOOR EXIT LIGHT LENS PER AMM 33-51-01

Part: BRACKET — LOOSE (GIRT BAR) · airframe 44,271 hrs · 24,577 cycles

L1 DOOR SLIDE HAS LOOSE RIVETS THAT ATTCH THE GIRT BAR FOR STOWAGE. / REMOVED, AND INSTALLED SERVICEABLE RIVETS ON L1 DOOR SLIDE GIRT BAR STOWAGE BRACKET IAW SRM 51-40-02-0G-0 STEP 4, AND AIPC 25-66-00-15.

Part: BRACKET — BROKEN (GIRT BAR) · airframe 44,271 hrs · 24,577 cycles

L2 DOOR SLIDE GIRT BAR STOWAGE BRACKET HAS 2 BROKEN RIVETS. / REMOVED, AND INSTALLED SERVICEABLE RIVETS ON L2 DOOR SLIDE GIRT BAR STOWAGE BRACKET IAW SRM 51-40-02-0G-0 STEP 4, AND AIPC 25-66-00-15.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 44,271 hrs · 24,577 cycles

FORWARD EMERGENCY EXIT LIGHT SPLICE LOCATED ON THE AFT WALL FORWARD LAV HAS A BENT PIN. / REPAIRED EMERGENCY EXIT LIGHT SPLICE IAW SOPM & AMM.

Part: FLOORBOARD — PULLED (NOT REPORTED) · airframe 44,271 hrs · 24,577 cycles

FLOOR PANEL 241 AF FIBERS PULLED OFF OF TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOORBOARD IAW B737 SRM 53-00-50-2R-0; PARA 1A (NOTE); 4A (TABLE 204); BOEING DWG #144A5810-127 & BAC5085- STEP (8.4.2.2)- REV E. RESIN CURED @ 150Ï¿½F FOR 1 HOUR USING HEAT LAMP & AAR TOOL #30347- DUE 05/08/20.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 44,271 hrs · 24,577 cycles

FLOOR PANEL 241DF FIBERS PULLED OFF OF TOP SURFACE FROM TAPE REMOVAL / REPLACED FLOOR PANEL 241DF BY FABRICATION NEW IAW B737 SRM 53-00-50-2R-0 REP GEN REV 69. DWG 144A5810-128 REV- AND BAC 5085 REV E

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 44,271 hrs · 24,577 cycles

CABIN FLOOR PANEL #241AEF, UPPER SIDE OF PANEL HAS AREAS OF FRAYING SKIN MATERIAL, MARKED IN BLUE REPAIRED PANEL 241AEF OF UPPPER FACESHEET DELAMINATION 14"X 4.25" IAW. B737-700 SRM 53-00-50-2R-1 SRM 53-00-50-2R-0 (A63278)(A89485) (A13438)(A67412)(A74475)(A29079)

Part: FLOOR PANEL — PULLED (NOT REPORTED) · airframe 44,271 hrs · 24,577 cycles

FLOOR PANEL 231 XF FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / REPLACED FLOOR BOARD BY FABRICATING NEW BOARD I/A/W 737-700 SRM 53-00-50-2R-0 GENERAL REV 69- DWG 144A5810 ID: 126 REV:-; BAC 5085 8.4.2.2.REV(E)

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 44,271 hrs · 24,577 cycles

CABIN FLOOR PANEL 242UF; UPPER SIDE OF PANEL; AREAS OF FRAYING ON UPPER SKIN PANEL / REPAIRED DAMAGE ON PANEL 242UF; BONDED REPAIR PLIES AND CURED TAP TEST GOOD IAW B737-700 SRM 53-00-50-2R-1 REV 69; SRM 53-00-50-2R-0 REV 69

Part: ANGLE — CORRODED (FUSELAGE) · airframe 44,271 hrs · 24,577 cycles

AFT CARGO PIT LEFT SIDE PLATE CORRODED BETWEEN BS 727+5 TO BS 767+15, LBL 21 ON UPPER SURFACE. R&R Z ANGLE IAW SRM & DWG.

Part: STRINGER FITTING — CORRODED (BS 360) · airframe 44,271 hrs · 24,577 cycles

ELECTRONICS & EQUIPMENT COMPARTMENT STRINGER END CORRODED AT BS. 360, STR. 28L. FITTING. / R&R FITTING IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 500A-500D) · airframe 44,271 hrs · 24,577 cycles

FORWARD CARGO PIT RIGHT SIDEPLATE STA 500A-500D RBL24 WL157 HAS CORROSION ON UPPER SURFACE / CORROSION AT STA 500A-500D RBL 24 WL 157 ON 'Z' ANGLE FOUND TO BE OUT OF LIMITS AT .040' ORIGNAL WITH .007' LOSS FOR A REMAINING THICKNESS OF.033' IAW SRM 53-00-53 FIG 103. REMOVED 'Z' ANGLE AND FABRICTION NEW PART IAW DRAWING 143A7501 REV A. FROM BAC 1496-444 7075-T6 ON A TAG #26081; INSTALLED IAW SRM 51-40-02 AND DRAWING #143A7500 REV-. P/N 1437501-186

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 44,271 hrs · 24,577 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140DF HAS CORROSION ALONG EDGES / CORROSION FOUND ON PNL 140DF. CORROSION REMOVED FROM PNL. CORROSION REMOVED RESULTED IN EXCEEDING 20 INCH MAX LENGTH IAW SRM 51-10-02; SRM 53-00-53-1A-1. NEW PNL MATERIAL VERIFIED IAW AIPC 25-52-10-02 AND DRAWING 453A2610 AS .071' 2024T3. NEW PNL FABRICATED; DRILLED AND TRIMMED IAW SRM 51-40-05-0G-0 AND DRAWING 453A2610 PNL TREATED; PRIMED AND CIC IAW AMM 51-00-58-201; AMM 51-21-72 AND 51-21-91

Part: ANGLE — DEFORMED (RT DOOR) · airframe 24,577 hrs · 44,271 cycles

PANEL 844DZ METAL ANGLE BENT/DEFORMED / REPLACED PANEL 844 DZ IAW AMM IPC 52-41-31-10; PG 11; ITEM 405 & AMM INTRODUCTION PGS 1 & 2. PAR 2.(A-B4)

Part: FITTING — CRACKED (NR 2 NACELLE) · airframe 44,271 hrs · 24,577 cycles

DURING F.O.M. INSPECTION OF THE #2 ENGINE AFT FAIRING FOUND THE AFT INBD WEB FITTING CRACKED / REMOVED AND REPLACED #2 ENGINE AFT FAIRING AFT EDGE P/N 313A2752-1 WITH ATAG WN6360 IAW AIPC 54-52-04-02; SRM 51-40-02 AND BOEING DWG 313A2400 REV C.

Part: ANGLE — BENT (DOOR) · airframe 24,577 hrs · 44,271 cycles

PANEL 834DZ METAL ANGLE BENT/DEFORMED / REPLACED PANEL 834 DZ IAW AMM INTRODUCTION; PGS 1 & 2; PAR 2(A-B4); AND IPC 52-13-21-10; PG 7. ITEM 110. REMOVED ATTACHED COMPONENTS; REPLACED PANEL 834 DZ A TAG: WN4160

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 44,271 hrs · 24,577 cycles

FWD CARGO DOOR SILL CENTER SCUFF PLATE IS CRACKED AT THE WELD; 8' FROM THE END. MARKED. / REPAIRED FWD CARGO DOOR CENTER SCUFF PLATE IAW EA 1-A53-2076; REV: 11. W/O 40452-1400-0001. PART TO BE INSTALLED ON EA 1-A53-2076; REV:11 W/O 40451-1400-0008-TASK 3(3). (J753-140-00-01Y)

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 43,747 hrs · 24,245 cycles

AFT RIGHT SLIDE NOT SECURE. / SECURED GIRT BAR TRIM PER MT.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 43,546 hrs · 24,119 cycles

AFT CARGO CENTER SCUFF PLATE DAMAGED. / REMOVED AND REPLACED SCUFF PLATE REF AMM 53-11-02 .

Part: LIGHT — UNSECURE (CABIN) · airframe 42,694 hrs · 23,553 cycles

PHOTO ILLUMINESCENT FLOOR LIGHT STRIP AT ROW 8 COMING UP. / SECURED STRIP PER AMM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 41,690 hrs · 22,898 cycles

EMERGENCY EXIT ROW WINDOW LIGHT INOP AIRCRAFT RIGHT. / RELAMPED PER AMM 33-51-01

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,913 hrs · 22,404 cycles

CENTER CABIN EMERGENCY AISLE LIGHT INOP AT LOCATION M2335. R&R BATTERY PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,913 hrs · 22,404 cycles

CENTER CABIN EMERGENCY AISLE LIGHT INOP AT LOCATION M1669. R&R BATTERY PER AMM.

Part: STRINGER — CRACKED (LT WING) · airframe 40,913 hrs · 22,404 cycles

LT WING STRINGER U10 CRACKED IN VERTICAL FLANGE AT WSTA 224.5 AT RIB 6. REPAIRED STRINGER IAW ER & EA.

Part: STRINGER — CRACKED (LT WING) · airframe 40,908 hrs · 22,403 cycles

LT WING STRINGER 10 CRACKED AT THE NR 6 RIB. REPAIRED STRINGER IAW EA.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 40,755 hrs · 22,302 cycles

R1 DOOR SLIDE INADVERTENTLY FELL OUT OF COMPARTMENT AT GATE. SECURED SLIDE PER IAW MM & MT.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 40,223 hrs · 21,938 cycles

AFT CARGO PIT FWD CORNER SCUFF PLATE CRACKED / CRACK ON AFT CARGO PIT; FWD CORNER SCUFF PLATE WAS WELDED IAW SWA EA 1-A53-2076; REV: 11

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 40,223 hrs · 21,938 cycles

AFT CARGO PIT AFT CORNER SCUFF PLATE CRACKED / ON AFT CARGOGO PIT; AFT CORNER SCUFF PLATE CRACK WELDED IAW SWA EA-1-A53-2076; REV: 11

Part: LATCH — LOOSE (L1 DOOR) · airframe 40,223 hrs · 21,938 cycles

L1 DOOR RT GIRT BAR LATCH LOOSE. SECURED LATCH IAW AMM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 40,223 hrs · 21,938 cycles

R1 DOOR NR 4 FRAME BEAM CRACKED IN BEAM AT INBOARD FORWARD CORNER OF BEAM BELOW DOOR HANDLE. R&R BEAM IAW SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 40,223 hrs · 21,938 cycles

R1 DOOR NR 5 FRAME BEAM CRACKED AT INBOARD FORWARD CORNER OF BEAM BELOW DOOR WINDOW. R&R BEAM IAW SRM AND ING DWG.

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 40,223 hrs · 21,938 cycles

CABIN FLOOR PANEL 241BF; UPPER SURFACE; INBD & OTBD SIDS; FACE SHEET PLYS PULLED LOOSE. / REPLACED CABIN FLOOR PANEL 241BF DUE TO FIBERS BEING DAMAGED THE ENTIRE LENGTH OF PANEL BY FABRICATING NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 REV. 65 FIG. 204; DWG 144A5910 REV A; AND BAC 5085 REV. E SECT. 8.4.22. CURED ADHESIVE FOR INSECTS @ 150 DEGREES F IN OVEN E0-01 DUE 10/20/18 IN: 11:30 OUT: 12:30. FLOOR PANEL BMS4-23 TYLL (A86949) INSERTS SL510713-410 (A83334) ADHESIVE EPI-420 (A93390)

Part: BRACKET — CRACKED (LT WING) · airframe 40,223 hrs · 21,938 cycles

LT. WING T.E. DEFLECTOR RIB SEAL RETAINER BRACKET IS CRACKED. / REMOVED AND REPLACED L/H WING T.E. DEFLECTOR RIB SEAL RETAINER BRACKET IAW B 737-700 DWG 115A2953 REV - SRM 51-40-02-0G-0

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 40,223 hrs · 21,938 cycles

CABIN FLOOR PANEL; 242AF UPPER SURFACE; INBD & OTBD SIDES; SOME FACE SHEET PLYS PULLED LOOSE. / FABRICATED NEW PANEL 242AF IAW SRM 53-00-50-2R-0 PARA 1A NOTE. USED EXISTING PANEL AS TEMPLATE. & IAW DWG 144A5810 ID0190 REV A

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 40,223 hrs · 21,938 cycles

FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED AT AFT END. / FWD CARGO COMP; FWD CORNER SCUFF PLATE WELDED ON SWA EA 1-A53-2076 REV:11.

Part: BATTERY — FAILED (CABIN) · airframe 39,936 hrs · 21,752 cycles

AFT RT EMERGENCY BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 39,928 hrs · 21,748 cycles

FORWARD LT EMERGENCY BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: BRACKET — BROKEN (LEFT WING) · airframe 37,810 hrs · 20,445 cycles

LEFT WING AFT UPPER TRAILING EDGE SHELF PANEL INNER BRACKET BROKEN ABOVE NACELLE STRUT FAIRING / REMOVED AND REPLACED BRACKET PER SRM 51-40-02

Part: BRACKET — CRACKED (LEFT WING) · airframe 37,810 hrs · 20,445 cycles

LEFT WING AFT UPPER TRAILING EDGE SHELF PANEL OUTER BRACKET CRACKED ATTACH TO SEAL RETAINER / REMOVED AND REPLACED BRACKET PER SRM 51-40-02

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 37,474 hrs · 20,230 cycles

RIGHT OVERWING EXIT LIGHT COVER MISSING. INSTALLED A COVER IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 36,218 hrs · 19,409 cycles

FWD CARGO DOOR SURROUND AFT SCUFF PLATE CRACKED / FWD CARGO AFT SCUFF PLATE RPEAIRED IAW EA 1-A53-2076 REV 11.

Part: STRAP — DAMAGED (FWD CARGO THRESH) · airframe 36,218 hrs · 19,409 cycles

LOGBOOK ENTRY REQUIRED - FORWARD CARGO DOOR SURROUND SKIN AND BEAR STRAP DAMAGED AT STA 440 S-22R / ACCOMPLISHED REPAIR TO FORWARD CARGO DOOR CUTOUT; SKIN AND BEAR STRAP; STAITON 440; STRINGER 22R REPAIRED IAW SRM 53-00-01-2R-25; REPAIR 25; FIGURE 202; DETAIL III AND AAR EA 170269 IR AND SWA EA 1-753-31432 IR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,073 hrs · 19,313 cycles

R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 35,734 hrs · 19,111 cycles

CAPTAINS WINDSHIELD HAD ARCED TOP OF WINDSHIELD. R&R L1 WINDOW PER MM.

Part: CONTROLLER — ARCED (WINDOW HEAT) · airframe 35,734 hrs · 19,111 cycles

CAPTAINS WINDSHIELD ARCED AT TOP OF WINDSHIELD. R&R HEAT CONTROLLER PER MM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 35,358 hrs · 18,876 cycles

R2 DOOR EXIT SIGN BY AFT GALLEY BROKEN. R & R THE SIGN IAW AMM.

Part: WIRE — DISCONNECTED (BATTERY PACK) · airframe 33,722 hrs · 17,888 cycles

EMERGENCY LIGHT BATTERY PACK DISCONNECTED AT BS 727C+13. CONNECTED BATTERY PACK IAW AMM.

Part: LENS — DIRTY (EMERGENCY LIGHT) · airframe 33,722 hrs · 17,888 cycles

LEFT WING TO BODY FAIRING AFT EMERGENCY LIGHT LENS DIRTY. CLEANED LENS IAW AMM.

Part: LENS — DIRTY (EMERGENCY LIGHT) · airframe 33,722 hrs · 17,888 cycles

RIGHT WING TO BODY FAIRING AFT EMERGENCY LIGHT LENS DIRTY. CLEANED LENS IAW AMM.

Part: LENS — DIRTY (EMERGENCY LIGHT) · airframe 33,722 hrs · 17,888 cycles

R2 DOOR AFT EMERGENCY LIGHT LENS DIRTY. CLEANED LENS IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 33,722 hrs · 17,888 cycles

FORWARD ENTRY LOWERED CEILING EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW SOPM.

Part: WINDOW FRAME — CRACKED (R1 WINDOW) · airframe 33,722 hrs · 17,888 cycles

FLIGHT DECK R1 WINDOW FRAME INNER CORNER CRACKED. REPAIRED THE WINDOW FRAME IAW ACO.

Part: PIN — LOOSE (R2 DOOR) · airframe 33,722 hrs · 17,888 cycles

RT EMERGENCY EXIT DOOR OPENING AFT UPPER DOOR STOP FITTING PIN LOOSE. SECURED PIN IAW AMM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 33,722 hrs · 17,888 cycles

R1 DOOR CUTOUT FWD STUB BEAM CRACKED AT BS 294.5, WL 210. R & R STUB BEAM IAW SRM.

Part: SLIDE — FRAYED (R2 DOOR) · airframe 33,722 hrs · 17,888 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT FRAYED. R & R SLIDE IAW MAINTENANCE.

Part: HOOK — CORRODED (CABIN) · airframe 33,722 hrs · 17,888 cycles

LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK CORRODED. R & R STRAP ASSEMBLY IAW AMM.

Part: HOOK — CORRODED (CABIN) · airframe 33,722 hrs · 17,888 cycles

RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK CORRODED. R & R STRAP ASSY IAW AMM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,722 hrs · 17,888 cycles

WEB CORRODED BETWEEN BS 947 TO BS 967, STR 20L. R & R WEB IAW DWG AND SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 33,722 hrs · 17,888 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM AND SRM.

Part: INTERCOSTAL — CORRODED (BS 986-1006) · airframe 33,722 hrs · 17,888 cycles

INTERCOSTAL WEB CORRODED BETWEEN BS. 986 TO BS. 1006, STRINGER 20L. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 33,722 hrs · 17,888 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH FORWARD FITTING CORRODED. R & R FITTING IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727D) · airframe 33,722 hrs · 17,888 cycles

AFT CARGO BAY R/H SIDEWALL SUPPORT CORRODED AT BS. 727D. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (BS 950-990) · airframe 33,722 hrs · 17,888 cycles

L2 DOOR THRESHOLD CREASE BEAM WEB CORRODED BETWEEN BS 950 TO 990, WL 208. R & R THE WEB IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (BS 294-312) · airframe 33,722 hrs · 17,888 cycles

INTERCOSTAL CRACKED BETWEEN BS. 294.5 TO BS. 312, RBL 16. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 33,722 hrs · 17,888 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO 344, LBL 47. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (BS 986-1006) · airframe 33,722 hrs · 17,888 cycles

INTERCOSTAL CORRODED BETWEEN BS 986 TO 1006, STR. 20L. R & R THE INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (BS 270-294) · airframe 33,722 hrs · 17,888 cycles

INTERCOSTAL CRACKED BETWEEN BS 270 TO 294.5, RBL 1. R & R THE INTERCOSTAL IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (BS 986) · airframe 33,722 hrs · 17,888 cycles

INTERCOSTAL TO FRAME ATTACH ANGLE CORRODED AT BS 986, STRINGER 20L. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 787) · airframe 33,722 hrs · 17,888 cycles

AFT CARGO BAY LEFT SIDEWALL SUPPORT CORRODED AT BS 787. R&R SUPPORT IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 33,722 hrs · 17,888 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19L. R & R GUSSET IAW SRM AND DWG.

Part: WINDOW FRAME — CRACKED (L1 WINDOW) · airframe 33,722 hrs · 17,888 cycles

FLIGHT DECK L1 WINDOW FRAME CRACKED AT UPPER OUTBOARD CORNER. REPAIRED FRAME IAW ER AND EA.

Part: WEB — CORRODED (THRESHOLD) · airframe 33,722 hrs · 17,888 cycles

AFT CARGO DOOR SUB THRESHOLD WEB CORRODED. R & R THE WEB IAW SRM.

Part: ANGLE — CORRODED (BS 867-947) · airframe 33,722 hrs · 17,888 cycles

AFT CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 867 TO 947. R & R THE ANGLE IAW SRM.

Part: SHIELD — CORRODED (BS 847-867) · airframe 33,722 hrs · 17,888 cycles

AFT CARGO BAY RIGHT SHIELD CORRODED BETWEEN BS 847 TO 867. R & R THE SHIELD IAW SRM.

Part: SUPPORT ANGLE — CORRODED (BULKHEAD) · airframe 33,722 hrs · 17,888 cycles

AFT CARGO BAY AFT CENTER BULKHEAD LOWER SUPPORT ANGLE CORRODED. R & R THE SUPPORT ANGLE IAW SRM.

Part: SPLICE PLATE — CORRODED (BS 887) · airframe 33,722 hrs · 17,888 cycles

AFT CARGO BAY BS 887 SPLICE PLATE CORRODED. R & R THE SPLICE PLATE IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 33,722 hrs · 17,888 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 33. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 33,722 hrs · 17,888 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: ANGLE — CORRODED (BS 500D) · airframe 33,722 hrs · 17,888 cycles

FORWARD CARGO BAY AFT BULKHEAD LOWER RT ANGLE CORRODED AT BS 500D, STRINGER 25R. R & R THE ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 500D) · airframe 33,722 hrs · 17,888 cycles

FORWARD CARGO BAY AFT BULKHEAD LOWER CENTER ANGLE CORRODED AT BS 500D, BETWEEN STRINGERS 25L - 25R. R & R THE ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 500D) · airframe 33,722 hrs · 17,888 cycles

FORWARD CARGO BAY AFT BULKHEAD LOWER LT ANGLE CORRODED AT BS 500D, BETWEEN STRINGERS 18 - 25L. R & R THE ANGLE IAW SRM.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 33,722 hrs · 17,888 cycles

CAPTAIN`S NR 1 WINDOW FRAME CORRODED ON EXTERNAL SURFACE AROUND PERIPHERY OF WINDOW FRAME. REPAIRED FRAME IAW EA.

Part: SIDEWALL SUPPORT — CORRODED (BS 492-500A) · airframe 33,722 hrs · 17,888 cycles

FORWARD CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 492 TO 500A, BETWEEN STRINGERS 24 - 25R. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 400-420) · airframe 33,722 hrs · 17,888 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO 420, STRINGER 25R. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 400-500D) · airframe 33,722 hrs · 17,888 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO 500D, STRINGER 25L. R & R THE SIDEWALL SUPPORT IAW SRM.